JP4576655B2 - COMPOSITE PRESSURE CONTAINER AND MANUFACTURING METHOD THEREOF - Google Patents
COMPOSITE PRESSURE CONTAINER AND MANUFACTURING METHOD THEREOF Download PDFInfo
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- JP4576655B2 JP4576655B2 JP2000027187A JP2000027187A JP4576655B2 JP 4576655 B2 JP4576655 B2 JP 4576655B2 JP 2000027187 A JP2000027187 A JP 2000027187A JP 2000027187 A JP2000027187 A JP 2000027187A JP 4576655 B2 JP4576655 B2 JP 4576655B2
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- JP
- Japan
- Prior art keywords
- inner liner
- resin
- layer
- pressure vessel
- modified epoxy
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Description
【0001】
【発明の属する技術分野】
この発明は、軽量で宇宙用気蓄器などに用いられる圧力容器等及びその製造方法に係り、更に詳しくは、高い破壊圧力を発現させた複合材圧力容器とその製造方法に関するものである。
【0002】
【従来の技術】
気体を蓄積する圧力容器としては、一般にスチール製が広く用いられており、消火器、窒素ガス容器、プロパンガス容器などが広く知られている。しかしスチール製容器は重いので用途によっては適用されない。例えば、特に軽量であることが要求される宇宙用気蓄器や航空機用途にはFRPを補強材に用いた複合材圧力容器が多く使用されている。その他、民生用としても例えば近年環境保護の点で注目されている天然ガス容器(NGV)には軽量な複合材圧力容器が適用されている。
【0003】
この種の圧力容器は、一般に非金属(主に樹脂)或いは金属製のインナライナの上にFRP層を設ける方法、また必要に応じてはウェット・フィラメントワインディングする方法等で製造されている。
【0004】
すなわち、例えば薄膜中空のチタニウム製のライナ(内層容器)の上に、エポキシ樹脂組成物を含浸したガラス繊維トゥ或いは炭素繊維トゥ等のフィラメント(補強繊維)をフープ巻き、ヘリカル巻き等により連続的に密に巻回することでフィラメントワインディングを行う。
【0005】
その後、所定時間、オーブン中で全体を加熱して硬化させ冷却させることにより各部を固化させることで繊維補強された複合材圧力容器が完成する。もちろん必要とされる強度が低いものについてはフィラメントワインディングは行わず単にFRP層のみを設けた構造も採用される。
【0006】
ところで、複合材圧力容器においては、複合材の保有する破断歪み以前で圧力容器が破壊する例も見られる。圧力破壊させた後の供試体を詳細に観察し、また応力解析の結果、想定値より低い圧力で破壊した圧力容器の場合には、金属ライナーと複合材層との間に間隙が生じると層間でスベリが発生していることが推定された。
【0007】
しかしながら、上述したような従来の方法においては、樹脂が室温で液状であるという制限があり、複合材料の機械的特性を高められない問題点があった。特に、高い機械的特性を発揮するトウプレグを使用した構造のものは内層の容器ライナと複合材層の間に“間隙”及び“スベリ”が生じ、本来の高い破壊圧力を発現できない欠点があった。
【0008】
【発明が解決しようとする課題】
この発明は、かかる従来技術の持つ課題に着目して案出されたもので、補強用の複合材層の効果を最大限に引き出して高い耐破壊圧力性能を発揮する軽量の複合材圧力容器を提供することを目的とするものである。
【0009】
【課題を解決するための手段】
上記課題を解決するために、本発明では、以下の構成の複合材圧力容器及びその製造方法を提供することである。
本願発明は、金属インナライナと該インナライナの外側にFRP層を有し、当該金属インナライナとFRP層との間に“間隙”及び“スベリ”が生じることを抑制すべく、該インナライナとFRP層との間に接着性に優れ且つ伸びの大きい熱可塑性樹脂層でありフェノキシ樹脂、ウレタン変性エポキシ樹脂及びナイロン変性エポキシ樹脂からなる群より選ばれる樹脂からなる樹脂層を介在させた複合材圧力容器にある。
また本願発明は、金属インナライナと該インナライナの外側にFRP層を有し、当該金属インナライナとFRP層との間に“間隙”及び“スベリ”が生じることを抑制すべく、該インナライナとFRP層との間に接着性に優れ且つ伸びの大きい熱可塑性樹脂層でありフェノキシ樹脂、ウレタン変性エポキシ樹脂及びナイロン変性エポキシ樹脂からなる群より選ばれる樹脂からなる樹脂層を介在させてトウプレグによりフィラメントワインディングした複合材圧力容器にもある。
更に本願発明は、金属インナライナと該インナライナの外側にFRP層を有し、当該金属インナライナとFRP層との間に“間隙”及び“スベリ”が生じることを抑制すべく、該インナライナとFRP層との間に接着性に優れ且つ伸びの大きい熱可塑性樹脂層でありフェノキシ樹脂、ウレタン変性エポキシ樹脂及びナイロン変性エポキシ樹脂からなる群より選ばれる樹脂からなる樹脂層を介在させる複合材圧力容器の製造方法にもある。
【0010】
このように接着性及び伸びの大きい熱可塑性樹脂を金属容器ライナと複合材層の間に介在させることにより、高い破壊圧力を発揮する軽量の圧力容器を提供することができる。
【0011】
【発明の実施の形態】
圧力破壊後の供試体を詳細に観察し、また応力解析の結果、低い圧力で破壊した複合材圧力容器では、金属ライナーと複合材層との間に間隙が生じると層間でスベリが発生しており、結果、複合材の保有する破断歪み以前で圧力容器が破壊に至ることが推定された。
【0012】
こうした、圧力破壊後の供試体の検証から、ライナーと複合材層との間に間隙が生じると層間でスベリが発生し強度を減じる結果となっていることが知られる。接着性に優れ、且つ、伸びの大きい樹脂を層間に介在させることが解決手段と考え、トウブレグに配合されているフェノキシ樹脂を塗布した結果、所定の成果をあげることが確認できた。
【0013】
従って、本発明では前述目的を達成するために、接着性及び伸びの大きい熱可塑性樹脂を容器ライナと複合材層の間に介在させる。これにより、圧力負荷印加時に発生する層間の間隙及びスベリが抑止されて高い破壊圧力を発揮する軽量の圧力容器が得られる。
【0014】
当該発明に適用して好適な樹脂としては、フェノキシ樹脂、ゴム変性エポキシ樹脂、ウレタン変性エポキシ樹脂、ナイロン変性エポキシ樹脂などが挙げられる。これ以外でも、金属ライナと複合材の層間に介在させ、接着性及び伸びに優れる樹脂であれば同様の効果を得ることができる。
【0015】
インナライナは金属ライナ以外でも良く同様の考えで非金属ライナにも適用することができる。金属ライナと複合材層との間にフェノキシレジンを介在させた構成の複合材圧力容器では、充分な強度を得ることができる。
【0016】
上記のような容器を製造するためには、例えば薄膜中空のチタニウム製のライナ(内層容器)を用意し、その上に、上記樹脂層を塗布し、更にエポキシ樹脂組成物を含浸したガラス繊維トゥ或いは炭素繊維トゥ等のFRP層を密に積層する。
【0017】
その後、所定時間、オーブン中で全体を加熱して硬化させ冷却させることにより各部を固化させることで繊維補強された複合材圧力容器が完成する。もちろんより強度が必要とされるものについてはフィラメントワインディングを行うようにしても良い。
【0018】
この場合には、例えば薄膜中空のチタニウム製のライナ(内層容器)を用意し、その上に、上記樹脂層を塗布し、更にエポキシ樹脂組成物を含浸したガラス繊維トゥ或いは炭素繊維トゥ等のフィラメント(補強繊維)をフープ巻き、ヘリカル巻き等により連続的に密に巻回することでフィラメントワインディングを行う。
【0019】
その後は、前述したと同様に所定時間、オーブン中で全体を加熱し、冷却させて複合材圧力容器を得る。
【0020】
このように本発明は、フェノキシレジンその他の樹脂を金属ライナまたは非金属ライナと複合材層との間に介在させる複合材圧力容器を構成することで、圧力負荷印加時に発生する層間の間隙及びスベリを防止してその耐破壊圧力を高めることを要旨とするものである。
【0021】
なお、本発明は宇宙用等の特殊用途だけでなく、NGV等の民生用にも利用できる。また、より大型構造の容器に適用することも可能である。
【0022】
〔実験例〕複合材圧力容器の前述層間に介在させる接着性に優れ且つ伸びの大きい樹脂をとして、トウプレグに配合されているフェノキシ樹脂を塗布した結果、所定の強度的成果をあげることができた。
【0023】
実施例1;チタニウム製ライナの上に、フェノキシ樹脂/MEK溶液を塗布し乾燥する。その上に、エポキシ樹脂組成物を含浸した炭素繊維トゥ(T800H東レ製)をフィラメントワインディングする。その後、180°C×3時間、オーブン中で加熱し硬化させて実施例の複合圧力容器を得た(供試体A)。
【0024】
比較例1;上記の製法から、フェノキシ樹脂/MEK溶液を塗布する工程を削除して比較例の複合圧力容器を得た(供試体B)。
【0025】
〔結果特性〕
供試体Aでは、439(kgf/cm^2 )の破壊圧力が得られた。
供試体Bでは、370(kgf/cm^2 )の破壊圧力であった。
【0026】
【発明の効果】
以上説明した如く、本発明方法によれば、軽量で破壊圧を発揮する複合材圧力容器を産業用或いは民生用途に提供することが出来る。[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a lightweight pressure vessel and the like used for space accumulators and the manufacturing method thereof, and more particularly, to a composite material pressure vessel expressing a high breaking pressure and a manufacturing method thereof.
[0002]
[Prior art]
As a pressure vessel for accumulating gas, generally made of steel is widely used, and a fire extinguisher, a nitrogen gas vessel, a propane gas vessel and the like are widely known. However, steel containers are heavy and are not applicable for some applications. For example, a composite pressure vessel using FRP as a reinforcing material is often used for space accumulators and aircraft applications that are particularly required to be lightweight. In addition, a lightweight composite pressure vessel is applied to a natural gas vessel (NGV) that has been attracting attention in recent years in terms of environmental protection for consumer use, for example.
[0003]
Pressure vessels of this type are generally non-metal are produced (mainly resin) or a method providing an FRP layer on the metal in Nara Ina, also optionally in a manner such as to wet filament winding.
[0004]
That is, for example, on the thin film hollow Titanium liner (inner case), full of glass fiber toe or carbon fiber-to-impregnated with the epoxy resin composition Iramento (reinforcing fibers) the hoop winding, continuously by helical winding, etc. Filament winding is performed by tightly winding the wire.
[0005]
After that, the composite material pressure vessel reinforced with fibers is completed by solidifying each part by heating the whole for a predetermined time to cure and cool. Of course, a structure in which only a FRP layer is provided without adopting filament winding is also used for those having low required strength.
[0006]
By the way, in the composite material pressure vessel, there is an example in which the pressure vessel breaks before the fracture strain possessed by the composite material. In the case of a pressure vessel that was broken at a pressure lower than the expected value as a result of stress analysis, the specimen after the pressure fracture was observed in detail, and if there was a gap between the metal liner and the composite material layer, It was estimated that slipping occurred.
[0007]
However, in the conventional methods as described above, there is a limitation that the resin is in a liquid state at room temperature, and there is a problem that the mechanical properties of the composite material cannot be improved. In particular, a structure using a tow prepreg that exhibits high mechanical properties has a defect that a “gap” and “slip” are generated between the inner container liner and the composite material layer, and the original high breaking pressure cannot be expressed. .
[0008]
[Problems to be solved by the invention]
The present invention was devised by paying attention to such problems of the prior art, and is a lightweight composite pressure vessel that maximizes the effect of the composite layer for reinforcement and exhibits high fracture pressure performance. It is intended to provide.
[0009]
[Means for Solving the Problems]
In order to solve the above-mentioned problems, the present invention is to provide a composite pressure vessel having the following configuration and a method for manufacturing the same.
The present invention has a metal inner liner and an FRP layer on the outer side of the inner liner. In order to suppress the occurrence of “gap” and “slip” between the metal inner liner and the FRP layer, the inner liner and the FRP layer adhesion excellent and elongation of the large thermoplastic resin layer der riff phenoxy resin between, the composite pressure vessel a resin layer interposed therebetween comprising a resin selected from the group consisting of urethane-modified epoxy resins and nylon modified epoxy resin is there.
The present invention also includes a metal inner liner and an FRP layer on the outer side of the inner liner, and the inner liner and the FRP layer are controlled to suppress the occurrence of “gap” and “slip” between the metal inner liner and the FRP layer. filament winding the adhesive excellent and elongation of the large thermoplastic resin layer der riffs phenoxy resin, by interposing a resin layer made of a resin selected from the group consisting of urethane-modified epoxy resins and nylon modified epoxy resin towpregs between There is also a composite pressure vessel.
The present invention further includes a metal inner liner and an FRP layer on the outer side of the inner liner, and the inner liner and the FRP layer are formed to suppress occurrence of “gap” and “slip” between the metal inner liner and the FRP layer. composite pressure vessel to interpose larger thermoplastic resin layer der riff phenoxy resin excellent and stretch adhesion, a resin layer composed of a resin selected from the group consisting of urethane-modified epoxy resins and nylon modified epoxy resin between the There is also a manufacturing method.
[0010]
Thus, by interposing a thermoplastic resin having high adhesion and elongation between the metal container liner and the composite material layer, a lightweight pressure container that exhibits a high breaking pressure can be provided.
[0011]
DETAILED DESCRIPTION OF THE INVENTION
The specimen after pressure fracture was observed in detail, and as a result of stress analysis, in a composite pressure vessel that was broken at low pressure, if a gap was generated between the metal liner and the composite layer, slipping occurred between the layers. As a result, it was estimated that the pressure vessel would break before the fracture strain of the composite material.
[0012]
From the verification of the specimen after the pressure fracture, it is known that when a gap is generated between the liner and the composite material layer, a slip is generated between the layers and the strength is reduced. It was confirmed that interposing a resin having excellent adhesiveness and large elongation between the layers was a solution, and as a result of applying the phenoxy resin blended in the toubreg, it was confirmed that a predetermined result was obtained.
[0013]
Therefore, in the present invention, in order to achieve the above object, a thermoplastic resin having high adhesiveness and elongation is interposed between the container liner and the composite material layer. As a result, a lightweight pressure vessel that exhibits high breaking pressure by suppressing gaps and slippage between layers generated when a pressure load is applied can be obtained.
[0014]
Examples of a resin suitable for application to the present invention include phenoxy resin, rubber-modified epoxy resin, urethane-modified epoxy resin, and nylon-modified epoxy resin. Other than this, a similar effect can be obtained as long as the resin is interposed between the metal liner and the composite material and has excellent adhesion and elongation.
[0015]
The inner liner may be other than a metal liner, and can be applied to a non-metal liner in the same way. A composite pressure vessel having a structure in which a phenoxy resin is interposed between a metal liner and a composite material layer can provide sufficient strength.
[0016]
In order to manufacture the container as described above, for example, a thin-film hollow titanium liner (inner layer container) is prepared, and the resin layer is applied on the liner and further impregnated with an epoxy resin composition. Alternatively, FRP layers such as carbon fiber tows are densely laminated.
[0017]
After that, the composite material pressure vessel reinforced with fibers is completed by solidifying each part by heating the whole for a predetermined time to cure and cool. Of course, filament winding may be performed for those requiring higher strength.
[0018]
In this case, prepared for example thin hollow Titanium liner (inner case), thereon, coating the resin layer, further off such as glass fiber toe or carbon fiber-to-impregnated with the epoxy resin composition Filament winding is performed by continuously and densely winding filaments (reinforcing fibers) by hoop winding, helical winding or the like.
[0019]
After that, as described above, the whole is heated in an oven for a predetermined time and cooled to obtain a composite pressure vessel.
[0020]
As described above, the present invention provides a composite material pressure vessel in which a phenoxy resin or other resin is interposed between a metal liner or a non-metallic liner and a composite material layer. The gist of this is to prevent the above and increase the breakdown pressure.
[0021]
The present invention can be used not only for special purposes such as space use but also for consumer use such as NGV. Moreover, it is also possible to apply to a container having a larger structure.
[0022]
[Experimental example] As a result of applying a phenoxy resin blended in toe prep as a resin having excellent adhesion and large elongation interposed between the aforementioned layers of the composite pressure vessel, a predetermined strength result was obtained. .
[0023]
Example 1 A phenoxy resin / MEK solution is applied on a titanium liner and dried. On top of that, carbon fiber toe (T800H Toray) impregnated with an epoxy resin composition is filament wound. Thereafter, the composite pressure vessel of the example was obtained by heating and curing in an oven at 180 ° C. for 3 hours (Sample A).
[0024]
Comparative Example 1: A composite pressure vessel of a comparative example was obtained by removing the step of applying the phenoxy resin / MEK solution from the above production method (Sample B).
[0025]
[Result characteristics]
For specimen A, a breaking pressure of 439 (kgf / cm ^ 2) was obtained.
Specimen B had a breaking pressure of 370 (kgf / cm ^ 2).
[0026]
【The invention's effect】
As described above, according to the method of the present invention, it is possible to provide a composite pressure vessel that is lightweight and exhibits a destructive pressure for industrial or consumer use.
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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JP2000027187A JP4576655B2 (en) | 2000-01-31 | 2000-01-31 | COMPOSITE PRESSURE CONTAINER AND MANUFACTURING METHOD THEREOF |
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JP2000027187A JP4576655B2 (en) | 2000-01-31 | 2000-01-31 | COMPOSITE PRESSURE CONTAINER AND MANUFACTURING METHOD THEREOF |
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JP2001214999A JP2001214999A (en) | 2001-08-10 |
JP4576655B2 true JP4576655B2 (en) | 2010-11-10 |
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Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
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JP2005337394A (en) * | 2004-05-27 | 2005-12-08 | Nippon Oil Corp | Fiber-reinforced pressure vessel, and its manufacturing method |
JP2008164131A (en) * | 2006-12-28 | 2008-07-17 | Nippon Polyethylene Kk | Pressure container and its manufacturing method |
DE102015203535B4 (en) * | 2015-02-27 | 2018-09-27 | Kautex Textron Gmbh & Co. Kg | Pressure vessel and method of manufacturing a pressure vessel |
JP6185117B2 (en) * | 2016-06-16 | 2017-08-23 | 八千代工業株式会社 | Manufacturing method of pressure vessel |
JP6923578B2 (en) * | 2019-02-25 | 2021-08-18 | 八千代工業株式会社 | Pressure vessel |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04119282A (en) * | 1990-05-25 | 1992-04-20 | Nkk Corp | Frp pipe and manufacture thereof |
JPH09112796A (en) * | 1995-10-12 | 1997-05-02 | Toyoda Gosei Co Ltd | Pressure container |
JPH10267195A (en) * | 1997-03-24 | 1998-10-09 | Kobe Steel Ltd | Lightweight pressure vessel |
Family Cites Families (1)
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JPH09280496A (en) * | 1996-04-18 | 1997-10-31 | Toray Ind Inc | Pressure vessel and its manufacture |
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Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04119282A (en) * | 1990-05-25 | 1992-04-20 | Nkk Corp | Frp pipe and manufacture thereof |
JPH09112796A (en) * | 1995-10-12 | 1997-05-02 | Toyoda Gosei Co Ltd | Pressure container |
JPH10267195A (en) * | 1997-03-24 | 1998-10-09 | Kobe Steel Ltd | Lightweight pressure vessel |
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